I am designing an orbital railgun simulator in MS Excel that should be able to propel a 20kg projectile to about 1% SoL. This would give 250 kT of TnT equivalent ( about 1TJ ) at ground zero.
I have already completed a simulator for the railgun and only need help with the ballistics of the projectile.
What I have :
Final Velocity ( +- 300 000 m/s )
Projectile Shape ( rod like ; much like the discarding sabot rounds that tanks use )
Projectile weight ( 20kg )
Projectile density ( tungsten carbide )
Air density ( assuming incompressible flow )
Total distance that projectile has to travel ( 2000 km )
Railgun simulator ( Can achieve any exit velocity )
What i need :
Exit velocity needed of the projectile from the barrel to achieve 1% SoL at ground zero.
As far as I understand, the flow regime will be turbulent all the way, and this is were I am stuck. I do not have a value for the drag coefficient of my projectile, but I did find a few values, but they are not for a rod-like shape with a sharp point.
I think I only need a Cd value for my equation then ill be fine and a equation for its contact area.
I can attach the railgun simulator if anyone would want it but it is not needed to solve the problem, it merely supplies the initial velocity.
Thank you for your time!

FB





